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Patent Searching and Data


Matches 301 - 350 out of 59,481

Document Document Title
WO/2018/033599A1
The invention relates to a seat arrangement, in particular designed to be installed in an airplane cabin, comprising: – at least one "front" seat unit (12) and at least one "rear" seat unit (12), positioned one behind the other along a...  
WO/2018/034142A1
With the present invention, flight plans are ascertained earlier in air traffic control. An air traffic control support system 3 includes a learning unit 100 and a prediction unit 200. The learning unit 100 generates a prediction model o...  
WO/2018/035544A3
In an illustrative embodiment, a frame assembly for enclosing an electronic device mounted to a rear surface of a seatback of an aircraft seat includes a rear frame for mounting within a recess of the rear surface of the seatback, a fron...  
WO/2018/031114A1
An Aerodrome providing safe storage for Unmanned Aerial Vehicles (UAVs) that includes an enclosure to protect UAVs from the elements (weather). The Aerodrome includes an enclosure, a foldable flight deck, a service interface, and a teles...  
WO/2018/028956A1
The present disclosure relates to a remote sensing system, comprising: an air towable housing for carrying one or more sensors, the air towable housing and/or a comprising at least a first pulley.  
WO/2018/027684A1
A mechanism for quickly folding and unfolding wings of an unmanned aerial vehicle, comprising an arm (1) and an arm mounting base (2); a guide post (20) is arranged on an upper surface of the arm mounting base (2), a sliding sleeve (21) ...  
WO/2018/030368A1
Disclosed is a probe capable of travelling, said probe having: wheels; a first camera disposed facing the direction in which the probe can travel; and a second camera disposed facing the directions except the direction in which the probe...  
WO/2018/029840A1
This probe, which is capable of travel, includes: wheels; a first camera disposed so as to face a direction in which the probe can travel; and a second camera disposed so as to face a direction other than the direction in which the probe...  
WO/2018/030722A1
A device and a method for controlling the pitch angle of a propeller are disclosed. According to one aspect of the present embodiment, one objective of the present invention is to provide the device and the method, which calculate the pi...  
WO/2018/029138A1
The invention relates to an unmanned aerial vehicle which is capable of hovering flight and can be coupled, reversibly and in a spatially fixed manner, to a surface of a structure being inspected, and which comprises at least one device ...  
WO/2018/029427A1
The invention relates to a projector (1) for light signalling, comprising - a conical mirror (16) having a truncated-cone shape (6), a plurality of laser diodes (5) emitting a light intensity towards the conical mirror (16), the inclinat...  
WO/2018/029841A1
The present invention includes: a first probe that includes a solar battery and that supplies electric power generated by the solar battery; and a second probe that probes natural resources by using the electric power supplied from the f...  
WO/2018/030651A1
Disclosed is an unmanned aerial vehicle comprising: a main body; a plurality of propeller connection parts extending from at least one side surface of the body at a specified length; a plurality of propellers respectively connected to th...  
WO/2018/027315A1
A lightweight, pocket-sized unmanned aerial vehicle (UAV) that can be held in an outstretched hand by a user for take-off and landing of the UAV. The UAV comprises a semi-toroidal or a substantially toroidal hollow body that defines a du...  
WO/2018/027338A1
Automatic terrain evaluation of landing surfaces, and associated systems and methods are disclosed herein. A representative method includes receiving a request to land a movable object and, in response to the request, identifying a targe...  
WO/2018/030880A3
An unmanned aerial vehicle according to an embodiment of the present invention comprises: a storage unit for storing information on a virtual fence (geo-fence) area, and flight approval information or photographing-approval information o...  
WO/2018/027686A1
A buffer mechanism for an unmanned aerial vehicle, comprising two stands (1) and a panel (2) for mounting the unmanned aerial vehicle, the panel (2) being provided thereon with holders (20) for holding the stands (1); a hollow cavity (21...  
WO/2018/031075A1
An aircraft includes a wing where a first rotor and a second rotor are coupled to the wing at a fixed position relative to the wing. The aircraft also includes a fuselage and a bearing. The bearing mechanically couples the wing and the f...  
WO/2018/031548A1
Engine mounting systems and methods that reduce engine core bending provide a first forward mount (130) connectable to a forward part of an engine core of an aircraft, an aft mount (150) connectable to an aft part of the core, and in a v...  
WO/2018/027682A1
A wing folding structure for an unmanned aerial vehicle, comprising an arm (1) and an arm mounting base (2), a blind hole (20) being provided on an end of the arm mounting base (2); also comprised is a connecting post (3) connected to a ...  
WO/2018/027925A1
A voltage distribution method and system for multiple motors of an unmanned aerial vehicle, the method comprising the following steps: detecting a wind power value of an unmanned aerial vehicle (S101); determining whether the wind power ...  
WO/2018/029227A1
The invention relates to the supply of a helicopter training device with electrical energy. The helicopter training device comprises a rotatable rotor which is driven by a local electric motor. The electric motor is supplied with electri...  
WO/2018/029119A1
The invention concerns a rotary-wing aerodyne (10), said aerodyne comprising: - a motor (35); - a structure (11) supporting at least one passenger seat; - a rotor (14) arranged above said structure (11) and linked to the motor by a hollo...  
WO/2018/028569A1
Disclosed is an ornithopter, with the specific structure of an airfoil being made into a single-side breathable structure. In the case where the airfoil flutters downwards, air does not pass through the airfoil, resistance is produced an...  
WO/2018/029406A1
The device comprises a sling (10) with four flexible support strands, including a pair of rear strands (11), each of which is attached by a bottom end to one of two lifting points provided in the lateral end portions of the transom stern...  
WO/2018/030367A1
The present invention has a first step for propelling, by electrical propulsion, a transport ship from a low earth orbit or a geostationary transfer orbit to a target orbit or destination.  
WO/2018/030880A2
An unmanned aerial vehicle according to an embodiment of the present invention comprises: a storage unit for storing information on a virtual fence (geo-fence) area, and flight approval information or photographing-approval information o...  
WO/2018/029739A1
It is desired that the heat generated by an imaging element with which an imaging device mounted in a mobile entity is provided be efficiently radiated. Or it is desired that a member for promoting the radiation of the heat generated by ...  
WO/2018/029833A1
The present invention has a step for exploring for a natural resource in a satellite, an asteroid, or a planet, a step for acquiring the natural resource detected by the exploration, and a step for storing the acquired natural resource.  
WO/2018/029839A1
The present invention relates to a transport method, a transport ship and a method for manufacturing a transport ship. The present invention has a first step for electrically propelling a transport ship to a lunar transfer orbit from a l...  
WO/2018/030649A1
The present invention provides a mobile terminal and a method of controlling the same. A mobile terminal according to an embodiment of the present invention includes a communication unit for transmitting/receiving data to/from a drone, a...  
WO/2018/027681A1
A foldable wing of a small unmanned aerial vehicle, comprising an arm (1) and an arm mounting base (2); an end of the arm mounting base (2) is provided with a blind hole (20) matching the arm (1); a first through hole (21) communicating ...  
WO/2018/027683A1
A quick disassembling and assembling wing of an unmanned aerial vehicle, comprising: a vehicle arm (1), and a vehicle arm installation base (2) provided with a first blind hole. The quick disassembling and assembling wing further compris...  
WO/2018/027685A1
A cushioning leg support for a small unmanned aerial vehicle, comprising a mounting base (1) and two supporting rods (2) which are arranged in parallel; arc connecting rods (3) are vertically and fixedly arranged on the supporting rods (...  
WO/2018/024915A1
Embodiments unmanned vehicles in which flight control sensors are carried in a stabilized head of the vehicle. Such stabilized flight control sensors experience less noise or generate less noise as a consequence of vehicle manoeuvring.  
WO/2018/026207A1
The present invention provides a motor for a drone, comprising: a rotary shaft; a stator including a hole in which a rotary shaft is arranged; and a rotor arranged on the outer side of the stator, wherein the rotor comprises: a cover par...  
WO/2018/027002A1
An aircraft where an engine creates mechanical energy. That energy is then converted into another transmittable form, e.g., electrical using a generator, or hydraulic using a pump, and is delivered to remotely-located motors and thruster...  
WO/2018/023366A1
A leading edge structure of a jet bridge floor, a jet bridge floor structure, and a jet bridge. The leading edge structure of a jet bridge floor comprises a reach assembly (1), a reach guide structure (2), and an energy storage assembly ...  
WO/2018/023555A1
Systems, methods, and/or devices are used for handling image data. An electronic device includes an imaging device, a storage device, and one or more processors coupled to the imaging device and the storage device. The electronic device ...  
WO/2018/023861A1
Provided in the present invention is a propeller (100), comprising blades (200). At a position on the blades (200), 46.875% from the center of gyration of the propeller (100), along the radius of gyration of the propeller (100), the angl...  
WO/2018/023854A1
An unmanned aerial vehicle-based external wall spray printing system and a spraying method therefor, wherein a spray nozzle is disposed on the unmanned aerial vehicle. The method comprises the following steps: A. controlling an unmanned ...  
WO/2018/027242A1
A system including a deployable barrier, a sensor to detect when to deploy the barrier and an activation device to deploy the barrier, wherein the barrier, sensor and activation device are connected a surface attached to a mobile device ...  
WO/2018/023869A1
Disclosed is a comprehensive service station for low-altitude aircrafts. The comprehensive service station comprises a dedicated exit, a dedicated entrance, a take-off and landing field, an energy supply zone, a navigation base station, ...  
WO/2018/026397A1
A propeller includes a blade free to rotate. A first stop is positioned to mechanically engage one or both of a first portion of the blade and a first structure coupled to the blade when the blade is in a first position at a first end of...  
WO/2018/023871A1
Disclosed is a low-altitude three-dimensional traffic system suitable for aerocars. The low-altitude three-dimensional traffic system comprises the aerocars, low-altitude routes for the aerocars, low-altitude comprehensive service statio...  
WO/2018/024310A1
It is an integrated system that (RECORD) registers the events on the plane (video/audio) and stored on the hard disk to get to know the truth of what happened on the aircraft in emergency situations and disasters and we can also get a li...  
WO/2018/024567A1
An assembly comprising a drone (1) and at least one releasable load (37) mounted on the drone, the drone comprising an on-board data processing system, the releasable load (37) comprising at least one sensor delivering a piece of informa...  
WO/2018/027017A1
A propulsion system for an aircraft includes an engine (e.g., piston engine, or turbine) having an axis made to be nonparallel with the longitudinal axis of the aircraft. This is enabled using an electrical, hydraulic, or other system to...  
WO/2018/025411A1
Provided is a novel cover for a small fixed-wing aircraft, wherein portions for protecting each section of the fuselage and portions for storing each of said portions are integrated, thereby allowing few persons, specifically, even a sin...  
WO/2018/024847A1
The invention relates to a system and method for distributing, delivering and collecting freight, having a number I of mobile freight stations (100), where I > 1, that each have a first interface (22) for automatically loading freight in...  

Matches 301 - 350 out of 59,481